EP0456737A1 - Stabilisateur a effet de bernoulli pour bande d'impression. - Google Patents

Stabilisateur a effet de bernoulli pour bande d'impression.

Info

Publication number
EP0456737A1
EP0456737A1 EP90903068A EP90903068A EP0456737A1 EP 0456737 A1 EP0456737 A1 EP 0456737A1 EP 90903068 A EP90903068 A EP 90903068A EP 90903068 A EP90903068 A EP 90903068A EP 0456737 A1 EP0456737 A1 EP 0456737A1
Authority
EP
European Patent Office
Prior art keywords
web
stabilizer
bar
air
field
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP90903068A
Other languages
German (de)
English (en)
Other versions
EP0456737B1 (fr
Inventor
Jeffrey W Sainio
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Quad Tech Inc
Original Assignee
Quad Tech Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Quad Tech Inc filed Critical Quad Tech Inc
Publication of EP0456737A1 publication Critical patent/EP0456737A1/fr
Application granted granted Critical
Publication of EP0456737B1 publication Critical patent/EP0456737B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B41—PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
    • B41F—PRINTING MACHINES OR PRESSES
    • B41F13/00—Common details of rotary presses or machines
    • B41F13/08—Cylinders
    • B41F13/10—Forme cylinders
    • B41F13/12—Registering devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B41—PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
    • B41F—PRINTING MACHINES OR PRESSES
    • B41F33/00—Indicating, counting, warning, control or safety devices
    • B41F33/0081—Devices for scanning register marks

Definitions

  • the present invention relates, generally, to mechanisms for stabilizing a moving web and to control systems for adjusting the color-to-color registration of multicolor web-fed printing press systems by stabilizing and optically scanning the web, and more particularly, to methods and apparatus for stabilizing the web without contact, thereby facilitating low depth- of-field scanning of the web in proximity to the print unit.
  • a web of material e.g., paper
  • a series of printing units each comprising a plate cylinder and a print cylinder (blanket cylinder) .
  • Each blanket cylinder contacts the web in sequence and applies a different color of ink thereto, which colors cooperate to imprint a multicolor image on the web.
  • the ink is still wet, and thus subject to smearing.
  • the web is typically routed through a drying unit to dry the image, heating the web to evaporate various solvents in the ink, then to a chill roller unit to cool the web and set the ink.
  • each blanket cylinder must be precisely aligned, i.e., proper registration of the respective colors must be maintained.
  • registration of the various print cylinders in multicolor systems was maintained manually.
  • a pressman would examine signatures (printed images) at the output of the press, and manually enter estimated lateral and rotational offset values into an electromechanical register control system to effect the necessary corrections. Maintenance of color registration in such systems requires the constant attention of the pressman since registration is often lost due to a number of uncontrollable variables in the web material and press hardware.
  • Automatic registration control systems for multicolor web-fed printing press systems are, in general, known.
  • commercially available closed loop register control systems utilize an optical scanning device cooperating with register marks printed on the web by the individual cylinders, to provide position feedback information indicative cf the registration of the respective print cylinders relative to a designated reference print cylinder.
  • each print cylinder produces a specific register mark forming part of a register pattern.
  • the optical sensor generates a signal indicative of the register pattern, which is analysed to determine the lateral and rotational registration of the respective print cylinders vis-a-vis the reference cylinder.
  • Registration error signals produced in accordance with the registration pattern, are employed to effect position correction of the respective print cylinders. Examples of such systems are described in EPO Application No. 87 104 973.0, filed April 3, 1987, and U.S. Serial No. 849,095, filed July 2, 1986 by the present inventor, both applications commonly assigned herewith.
  • Optimal scanning accuracy may be achieved when the web is scanned under conditions yielding relatively little web "weave” (spurious lateral movement of the web, e.g., movement transverse to the direction of web travel, in the plane of the web) and "flutter” (spurious movement of the web in a direction perpendicular to the plane of the web) .
  • Preprinted control marks are preferably as small and unobtrusive as possible.
  • the ability of the scanner to accurately detect the presence and position of a mark tends to be inversely proportional to mark size; the smaller the mark, the more likely that misregistration or web weave will take the mark outside of the field of view of the scanner.
  • optical scanners tend to have a relatively limited depth-of-field, i.e., they are capable of accurately sensing only those images within a predetermined range of distance from the scanner, typically on the order of approximately 0.025 inches.
  • web flutter in the vicinity of the scanner should be maintained within the limits of the scanner depth- of-field.
  • flutter is typically maintained within acceptable limits by physically restraining the web, e.g., scanning the web as it wraps around an idler roller, or the like, or in the vicinity of such a wrap.
  • misregistration be detected as quickly as possible after printing, i.e., that the web be scanned as early in the process after the printing operation as possible.
  • high web speeds e.g. 2000 feet per minute
  • relatively short delays in detecting misregistration can cause considerable wastage.
  • a principal source of web flutter is observed at the line of contact between the web and the final print cylinder as the web leaves the printing stage.
  • the ink applied to the web by the print cylinder is tacky when moist, causing the web to adhere to the outer circumference of the print cylinder.
  • the adhesion In regions of high image density, the adhesion is relatively strong; in regions of low image density, the adhesion is relatively weak.
  • Localized fluctuations in web tension as the web is pulled from the print cylinder surface cause the web to flutter with an amplitude in the range of about 3/16 to 1/4 inch in the vicinity of the final print cylinder, far beyond the maximum depth-of-field variations tolerated by commercially available scanners (e.g. .025 inches).
  • flutter amplitude must be reduced by approximately a factor of ten between the point at which the web leaves the print cylinders and the point at which the web surface is scanned.
  • various web characteristics can cause the web to dry at different rates along the length thereof, resulting in non-uniform shrinkage or expansion of the web. This can result in web weave, on the order of about 1/2 inch. This is compounded by periodic cleaning of the blanket cylinders (known as a "blanket wash") .
  • a blanket wash obliterates registration marks, and often makes the web weave; the marks disappear, then reappear in a different lateral location due to the web weave caused by the blanket wash.
  • the register control system almost invariably loses "track” of the mark, and must reacquire the mark after a blanket wash. This, of course, delays correction of misregistration.
  • a web typically travels between 100 and 160 feet between the point at which the web emerges from the printing units and the point at which the web emerges from the dryer. Considerable wastage results from the delay in detecting misregistration. Thus, a technique is needed for stablizing the web, without contact, prior to the drying operation.
  • Tec Systems Tec-Turn(R) which turns a web of paper approximately 90 degrees upward into an overhead dryer.
  • the Tec-Turn unit is adequate for turning, but the distance from the a outlet to the paper may vary from a few hundredths of an inch to 1/4 inch, depending on paper tension and air pressure. This is adequate for turning the paper but inadequate for keeping the paper within the practical focusing range of a scanner.
  • the present invention facilitates enhanced closed loop register control by stabilizing the printed web as it leaves the final print cylinder, thereby allowing tighter control of color-to-color registration by minimizing the amount of web travel between the printing operation and the scanning operation.
  • a Bernoulli-effect stablizer is disposed proximate the point at which the web leaves the print cylinders.
  • FIGURE 1 is a block schematic front elevation view of a printing system in accordance with the present invention j
  • FIGURE 2 is a block schematic top plan view of the printing press of FIGURE 1;
  • FIGURE 3 is a top plan view of the stabilizer of FIGURES 1 and 2;
  • FIGURE 4 is a cross-section view of the stabilizer shown along line IV-IV of FIGURE 3;
  • FIGURE 5 is a cross-section view of the stabilizer shown mounted to the press taken along line V-V of FIGURE 2;
  • FIGURE 6 is an enlarged view of the stablizer of FIGURES 3-5 shown interacting with a moving web;
  • FIGURE 7 is a top plan view of an alternate embodiment of the stabilizer of FIGURES l and 2;
  • FIGURE 8 is a cross-section view of the stablizer shown along line VIII-VIII of FIGURE 7;
  • FIGURE 9 is an enlarged view of the stabilizer of FIGURES 7-8 shown interacting with a moving web.
  • a web-fed printing system 100 preferably including a printing press 101 and comprising a plurality of serially disposed conventional printing units 102, 103, 104, and 105, operates upon a driven web 110.
  • each of printing units 102-105 advantageously includes an upper blanket cylinder 116, an upper plate cylinder 117, a lower blanket cylinder 118, and a lower plate cylinder 119.
  • Web 110 typically paper, is fed from a reel stand 120 through each of printing units 102-105 in sequence and thereafter through a dryer unit 112 and chill unit 114. Web 110 is then suitably guided through a coating unit 122 and a folding station 124 which folds and separates the web into individual signatures.
  • Printing units 102-105 cooperate to imprint multicolor images on the upper and lower surfaces of web 110.
  • Each printing unit 102-105 prints an associated color of ink; typically the first sequential print unit 102 prints the color black, and subsequent units 103-105 print other colors such as cyan, magenta, and yellow.
  • Print unit 105 is referred to herein as the terminal print unit.
  • Each of the lateral and rotational positions of upper and lower plate cylinders 117, 119 is separately controlled by electric motors (not shown) to precisely register the respective images generated by the individual printing units.
  • a non-invasive stabilizer is employed to facilitate scanning of the web, between the individual printing units 102-105, immediately upon exit from press 101, or otherwise between press 101 and dryer 112.
  • a non-invasive stabilizer 130 is advantageously mounted to a side frame 129 of printing press 101.
  • Register qontrol system 170 provides appropriate signals to the electric motors of the plate cylinders to precisely control lateral and rotational position of the upper and lower plate cylinders, respectively.
  • Stabilizer 130 can be any mechanism which dampens flutter of web 110 to within acceptable limits for scanning (i.e., within the depth-of-field of units 131A, 131B) , without causing the image imprinted on the respective surfaces of web 110 to smear.
  • Stabilizer 130 can, for example, comprise respective forced-air conduits, disposed on either side of web 110, including apertures to generate respective oppositely directed air streams impinging on both the upper and lower surface of web 110 with sufficient force to stabilize the web.
  • stabilizer 130 employs a Bernoulli-effect to stabilize web 110.
  • stabilizer 130 preferably comprises a forced air conduit bar 132 disposed transverse to the direction of web travel, extending across the width of web 110.
  • Stabilizer 130 directs a stream of pressurized air, transverse to the plane of the web, against the surface of the web.
  • This high velocity air creates a zone of reduced static pressure adjacent the surface of the web, thereby pulling the web toward the stabilizer.
  • the outward pressure of the forced air in conjunction with the pocket of high velocity air trapped between the web surface and the stabilizer surface, prevents the web from contacting the stabilizer.
  • a plurality of stabilizer units may be simultaneously employed, for example, above and below the web, as desired.
  • the preferred embodiment will be described in the context of a single stabilizer disposed underneath the web.
  • conduit bar 132 is suitably square in cross-section and of a length, e.g., 52 inches, in excess of the width of web 110.
  • a hollow interior chamber 138 spans the length of the bar, the cross-sectional area of chamber 138 being sufficient to accomodate a desired air flow, suitably on the order of 2 to 10 PSI, preferably within the range of 2 to 4 PSI.
  • Chamber 138 communicates with a compressed air source (not shown) through an air inlet junction 140 suitably disposed at an end of bar 132.
  • a controlled air stream outflow is provided from the surface of conduit bar 132 facing web 110.
  • a series of air discharge holes 142 are formed through the wall of bar 132 along the length of bar 132.
  • Respective gap adjusting strips 134 and 136 are secured to the surface of bar 132. Adjusting strips 134 and 136 cooperate to define a linear gap 144 therebetween generally overlying holes 142, preferably of a length corresponding to the width of web 110. Holes 142 and gap 144 define the path of discharged air from conduit bar 132, and thus the air stream against web 110.
  • the use of holes 142, and overlying strips 134, 136, to provide and control the air flow is particularly advantageous; it provides a structure mechanically strong enough to operate at relatively high air pressures without deformation of the air outlet.
  • the square cross section of conduit 132 facilitates formation of holes 142, and the securing of strips 134 and 136.
  • width of gap 144 allows precise control over the velocity of the discharge air passing therethrough. For a given air pressure within chamber 138, decreasing the width of gap 144 increases the discharge air speed; conversely, increasing the width of gap 144 decreases the discharge air speed.
  • gap 144 is preferably such that gap 144 provides a significant resistance to air flow, greatly in excess of the resistance generated by the presence of web 110 in the vicinity of gap 144.
  • air flow through gap 144 will be substantially constant across the length of the gap whether or not web 110 extends across the entire length of gap 144.
  • Webs of varying widths are therefore readily accomodated; gap 144 is of a length corresponding to the widest web contemplated to be encountered.
  • the width of gap 144 is suitably on the order of eight to fifteen thousandths of an inch (0.008 to 0.015 inch).
  • Strip 134 is secured to bar 132 in any convenient manner, for example by bolts 146. Alternatively, strip 134 may be held in place by screws, welding, or may be formed integral with bar 132, as desired. Adjusting strip 136, on the other hand, is preferably slideably secured to bar 132, for example by respective slotted screws 148 received within slots 150. In this way, the width of gap 144 may be adjusted by disposing and securing strip 136 at a predetermined desired distance from strip 134. Of course, if desired, both strips 134 and 136 may be fixedly secured to conduit bar 132.
  • stabilizer apparatus 130 is advantageously mounted to press 101 near the point at which web 110 leaves press 101.
  • a mounting member 154 is affixed to press frame 129, for example, by an upper bolt 156 and a lower bolt 160.
  • An L-shaped bracket 158 is secured to mounting member 154, for example by bolt 156 and a medial bolt 162.
  • Bar 132 of stabilizer 130 is received within L- shaped bracket 158 and secured thereto by, for example, one or both of bolts 156 and 162.
  • Mounting member 154 and L-shaped bracket 158 suitably span approximately the entire length of bar 132, and a plurality of bolts 156, 160, and 162, spaced apart along the length of mounting member 154, may be used as necessary.
  • Scanner 13IB is suitably mounted to sidewall 129 of press 101, or to mounting bracket 154, and disposed to focuse upon an area of web 110 in the vicinity of stabilizer 130.
  • Scanner 13IB is suitably focused on an area of the web within, e.g., five or six inches from stabilizer 130.
  • Scanner 131A is suitably mounted to the side of press 101 on the opposite side of web 110 from stabilizer 130.
  • Scanner 131A is suitably focused on a portion of web 110 overlying stabilizer 130.
  • the point of focus is preferably not directly over gap 144; there tends to be little if any Bernoulli effect immediately overlying gap 144, causing a slight pucker in the web immediately above gap 144. Accordingly, the point of focus preferably overlies one of adjusting bars 134 or 136.
  • stabilizer 130 is advantageously mounted such that the upper surfaces of respective adjusting strips 134 and 136 are disposed approximately 3/16 of an inch from web 110 when the stabilizer is in the off condition.
  • compressed air is forced upwardly through respective holes 142 and gap 144, ultimately impinging upon the downward facing surface of web 110.
  • the pressure of the discharged air which is confined between the upper surfaces of strips 134, 136 and the underside of web 110 creates a cushion of horizontally moving air; the velocity of this air creates a zone of reduced static pressure between the stabilizer and the web in accordance with the Bernoulli principle.
  • the static pressure above the web, f course, remains unaffected by the operation of the stabilizer.
  • an __ alternate exemplary embodiment of the stabilizer bar in accordance with the present invention suitably comprises respective gap adjusting strips 202 and 204 defining an angled air gap 206 therebetween.
  • Gap adjusting strip 204 is suitably secured to conduit bar 132 by slotted screw 148 received within slot 150, as described above in connection with strip 136.
  • Gap adjusting strip 204 advantageously comprises an angled portion 210 defining an acute angle with the surface of conduit bar 132 upon which respective holes 208 are disposed.
  • Gap adjusting strip 202 is advantageously secured to conduit bar 132 in any convenient manner, for example by bolts 146.
  • a spacer 212 is advantageously disposed intermediate gap adjusting strip 202 and conduit bar 132 such that, when stabilizer 130 is mounted to side frame 129 of press 101 as depicted in FIGURE 9, the height of gap adjusting strip 202-exceeds that of strip 204 by an amount approximately equal to the thickness of spacer 212, for example, approximately .060 inches.
  • strip 202 suitably comprises an inclined portion 214 defining the downstream edge of gap 206; angled portion 210 of strip 204 comprises the upstream edge of gap 206.
  • the stream of discharged air from stabilizer 130 impinges web 110 at an acute angle with respect to the plane of travel of web 110.
  • a relatively insignificant amount of discharge air enters the region between the web and the upper surface of strip 204, the majority of the discharge air being directed between the web and strip 202. Consequently, the Bernoulli effect is largely confined to that portion of stabilizer 130 downstream of gap 206.
  • any debris which may fall from the web for example sputtered ink, dust, and the like, will thus be blown downstream by the airstream discharged from gap 206.
  • strip 204 To avoid contact between strip 204 and web 110' when web 110' is in the control (stabilization) zone, i.e., approximately .007 inches from adjusting strip 202 during operation of stabilizer 130, it is advantageous for strip 204 to be disposed out of (beneath) the control zone by an amount approximately equal to the thickness of spacer 21.
  • the web stablizer need not be secured to the side frame of the printing press; the stabilizer may be disposed at any convenient point along the web path, although proximity to the source of flutter, i.e., the print cylinders, is advan ⁇ tageous.
  • the preferred embodiment employs a Bernoulli-effect stabilizer, any suitable technique for dampening web flutter which does not smear the ink is satisfactory.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Inking, Control Or Cleaning Of Printing Machines (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Investigating Or Analysing Biological Materials (AREA)
  • Bidet-Like Cleaning Device And Other Flush Toilet Accessories (AREA)
  • Registering, Tensioning, Guiding Webs, And Rollers Therefor (AREA)
  • Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)
  • Materials For Medical Uses (AREA)

Abstract

Le système et le procédé décrits, servent à générer des indications d'erreurs d'alignement entre des unités d'impression respectives séparément réglables d'une presse d'imprimerie. Les unités d'impression coopèrent de façon à imprimer une image sur une bande en mouvement. Le système est du type comprenant une commande photo-optique, qui présente un champ optique et une profondeur de champ et qui sert à générer des signaux de sortie indicateurs d'une disposition relative prédéterminée des marques sur la bande traversant le champ optique à l'intérieur de la profondeur de champ de la commande photo-optique, pendant le mouvement de la bande par rapport aux unités d'impression, ainsi que des circuits processeurs, qui réagissent aux signaux de sortie photo-optiques et qui servent à générer des signaux indicateurs des déviations des marques d'alignement imprimées par les unités d'impression par rapport à la disposition relative prédéterminée. Le système et le procédé décrits se caractérisent en ce que: la commande photo-optique est disposée à proximité des unités d'impression et en ce qu'une structure stabilisatrice à entraînement pneumatique est associée à la commande photo-optique et sert à maintenir la bande dans la profondeur de champ grâce à la création d'un effet de Bernoulli.
EP90903068A 1989-04-19 1990-01-09 Stabilisateur a effet de bernoulli pour bande d'impression Expired - Lifetime EP0456737B1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US07/340,498 US4913049A (en) 1989-04-19 1989-04-19 Bernoulli-effect web stabilizer
US340498 1989-04-19
PCT/US1990/000189 WO1990012689A1 (fr) 1989-04-19 1990-01-09 Stabilisateur a effet de bernoulli pour bande d'impression

Publications (2)

Publication Number Publication Date
EP0456737A1 true EP0456737A1 (fr) 1991-11-21
EP0456737B1 EP0456737B1 (fr) 1995-04-05

Family

ID=23333620

Family Applications (1)

Application Number Title Priority Date Filing Date
EP90903068A Expired - Lifetime EP0456737B1 (fr) 1989-04-19 1990-01-09 Stabilisateur a effet de bernoulli pour bande d'impression

Country Status (7)

Country Link
US (1) US4913049A (fr)
EP (1) EP0456737B1 (fr)
AT (1) ATE120693T1 (fr)
AU (1) AU5092490A (fr)
CA (1) CA2007844A1 (fr)
DE (1) DE69018449T2 (fr)
WO (1) WO1990012689A1 (fr)

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US6619354B1 (en) 1998-12-17 2003-09-16 Bridgestone Corporation Run flat pneumatic tire with shoulder cushion rubber layer loss tangent less than carcass coating rubber loss tangent

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GB8823815D0 (en) * 1988-10-11 1988-11-16 Molins Plc Pneumatic web feeding
US5640835A (en) * 1991-10-16 1997-06-24 Muscoplat; Richard Multiple envelope with integrally formed and printed contents and return envelope
US5412577A (en) * 1992-10-28 1995-05-02 Quad/Tech International Color registration system for a printing press
US6298782B1 (en) 1993-03-25 2001-10-09 Baldwin Web Controls Anti-wrap device for a web press
US5678484A (en) * 1993-03-25 1997-10-21 Baldwin Web Controls Anti-wrap device for a web press
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US5813337A (en) * 1996-06-05 1998-09-29 Quad/Tech, Inc. Closed-loop printing control system
US5967457A (en) * 1996-07-23 1999-10-19 Thermo Wisconsin, Inc. Airfoil web stabilization and turning apparatus and method
US5857784A (en) * 1997-01-28 1999-01-12 Bayer Corp. Agfa Division Image position error detection technique
US6164847A (en) * 1997-01-28 2000-12-26 Agfa Corporation Imaging parameter detection
US6535307B1 (en) 1997-02-13 2003-03-18 Agfa Corporation Method and apparatus for display of imaging parameters
US6721061B1 (en) 1997-02-13 2004-04-13 Agfa Corporation Method and apparatus for display of banding
US6810813B2 (en) * 2003-03-14 2004-11-02 Heidelberger Druckmaschinen Ag Device and method for controlling registration in a printing press
US20040213436A1 (en) 2003-04-25 2004-10-28 Quad/Tech, Inc. System and method for measuring color on a printing press
US6942175B2 (en) * 2003-06-12 2005-09-13 Joseph A. Watkins Winding apparatus having Bernoulli guide shoe leading into roller-core nip and method
DE102004033096B4 (de) * 2004-07-08 2008-02-07 Lsc Prozess- Und Laborsysteme Gmbh Materialbahn-Inspektionsanlage
US9399531B2 (en) * 2005-10-25 2016-07-26 Formax, Inc. Sheet interleaver for slicing apparatus
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WO2018017712A1 (fr) 2016-07-20 2018-01-25 Ball Corporation Système et procédé permettant d'aligner un dispositif d'encrage d'un dispositif de décoration
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6619354B1 (en) 1998-12-17 2003-09-16 Bridgestone Corporation Run flat pneumatic tire with shoulder cushion rubber layer loss tangent less than carcass coating rubber loss tangent
US6889736B2 (en) 1998-12-17 2005-05-10 Bridgestone Corporation Run flat pneumatic tire with shoulder cushion rubber layer loss tangent less than carcass coating rubber loss tangent
US7195046B2 (en) 1998-12-17 2007-03-27 Bridgestone Corporation Run flat pneumatic tire with shoulder cushion rubber layer loss tangent less than carcass coating rubber loss tangent

Also Published As

Publication number Publication date
EP0456737B1 (fr) 1995-04-05
DE69018449T2 (de) 1995-10-19
DE69018449D1 (de) 1995-05-11
AU5092490A (en) 1990-11-16
US4913049A (en) 1990-04-03
CA2007844A1 (fr) 1990-10-19
ATE120693T1 (de) 1995-04-15
WO1990012689A1 (fr) 1990-11-01

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